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Studies have demonstrated that heating leads to an increased boundary layer thickness and upstream shock movement, which in turn exacerbates separation and enlarges the recirculation region [2].
An account is given of an investigation into the interaction between the boundary layer on a flat plate and a shock wave produced either externally, by a wedge in the supersonic main-stream, or from ...
Kevin Posladek, a PhD candidate in mechanical engineering, began his work in the Hypersonics Lab working under advisor and ...
We have found that low levels of helium injection near the leading edge stabilizes the turbulent boundary layer, apparently causing a reverse transition to laminar flow to take place. These results ...
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